Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
  • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
  • F15D1/00—Influencing flow of fluids
  • F15D1/02—Influencing flow of fluids in pipes or conduits
  • F15D1/06—Influencing flow of fluids in pipes or conduits by influencing the boundary layer
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
  • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
  • F15D1/00—Influencing flow of fluids
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64C—AEROPLANES; HELICOPTERS
  • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F42—AMMUNITION; BLASTING
  • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
  • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
  • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
  • F42B10/38—Range-increasing arrangements

Definitions

• This invention relates to a method for controlling turbulence in a fluid medium including, for example, turbulence created by relative movement between a body and a fluid medium, or by a shear flow between two fluids.
• a fundamental property of developed turbulence is that, although most of the energy of turbulent motion is associated with large scales, the dissipation of energy as a consequence of the turbulent motion occurs at small scales comparable to the Kolmogoroff length scale. Such dissipation is manifested by the conversion of molecular movement into heat, and this viscous dissipation takes place mainly in the boundary layer in a fluid medium which exists between a body and the fluid, or between, for example, two fluids of different densities.
• the inertial range Between the large scales where turbulent motion occurs, and the small scales where dissipation of energy occurs, lie intermediate scales often referred to as the inertial range. Energy is transmitted from the non-dissipative large scales to the dissipative small scales through the inertial range scales which thus serve as an energy transmission bridge.
• the dissipation of energy due to turbulence e.g., turbulence created by relative movement between a body and a medium is manifested in different ways.
• the dissipation is evidenced by downstream pressure loss; in the case of aircraft flight, or underwater submarine movement, the dissipation is evidenced by increased drag.
• Flame propagation, and heat transfer associated with turbine blades, as well as often violent, geophysical phenomena such as tornadoes may constitute additional modalities in which energy injected at relatively large scales, is dissipated due to turbulent flow at small scales.
• the present invention controls turbulence in a fluid medium by introducing a broad spectrum stochastic external disturbance into the medium. It is presently believed that this has the effect of disrupting the coherence in the inertial range and interrupting the ability of the inertial range to conduct energy from the large scales to the viscous scales where energy dissipation takes place. As a consequence, energy remains at the large scales, and viscous dissipation at small scales is reduced because less energy is supplied.
• the present invention includes introducing the disturbance into the medium via the boundary layer.
• the spectrum of said disturbance includes wavelengths in the inertial and dissipative subrange length scales.
• the spectrum of said disturbance should include wavelengths at least greater than the dissipative subrange length scale.
• the wavelengths of said disturbance are comparable to, or larger than, the Kolmogoroff length scale.
• the maximum wavelengths of said disturbance are comparable to the Taylor microscale or even larger scales in the inertial range.
• the disturbance may be an essentially white noise signal that may be modulated.
• One of the techniques for introducing the required disturbance is to inject an essentially white noise signal into the boundary layer of the medium adjacent to the body such that the signal is coupled to and perturbs the medium.
• Such signal is temporally and spatially random and serves to introduce chaotic elements into the medium at a location where the wavelength of the perturbing signal is comparable to the dissipation length scale which is related to the scale of the energy containing eddies in the motion. That is to say, the average wavelength of the perturbing signal is comparable to the size of the eddies in the viscous sublayer portion of the boundary layer.
• the average wavelength of the perturbing signal can be substantially equal to the Kolmogoroff length scale for the flow.
• the average wavelength can be substantially equal to the Taylor microscale. In such a case, the effect will be larger.
• the invention is applicable to the operation of a vessel in a body of fluid, such as a submarine under water, an aircraft in the atmosphere, or to the control of other turbulent shear flows and homogeneous turbulence.
• a vessel in a body of fluid such as a submarine under water, an aircraft in the atmosphere
• an essentially white noise disturbance is introduced into the boundary layer of the fluid adjacent the vessel, the central frequency of the noise being chosen to enhance propulsion of the vessel in the body of fluid by introducing a chaotic perturbation into the boundary layer.
• the dynamics of coherent patterns or structures in the turbulence by which energy is transferred in cascade fashion from larger eddies to smaller eddies (i.e., from a region of small wave numbers in the flow to a region of large wave numbers), can be destroyed by small scale, high frequency forcing.
• coupling of the external signal to the fluid for effecting its perturbation can be achieved by creating an appropriate randomly varying in time and space electromagnetic field in the boundary layer adjacent to the skin of the vessel.
• coupling can be achieved by creating an appropriately varying time and space sonic field within the boundary layer.
• Such turbulence can be thought of as a mechanism which converts low entropy energy present in large eddies with a few degrees of freedom into high entropy energy present in small eddies with a large number of degrees of freedom.
• turbulent dissipation results in an energy cascade that produces high entropy energy that is disposed of in the small dissipation scales
• turbulent dissipation predominately takes place in the viscous sublayer (i.e., dimensions associated with regions of the flow within which molecular interactions result in the dissipation of turbulent energy).
• Coherent organization of large scales in the turbulent flow is sustained by disposal of the accumulation of high entropy energy. In other words, a long range topological order is induced by energy dissipation at small scales, at the same time that chaos is precluded.
• turbulence is inseparable from the vortex line stretching process which in turn implies a growth in the surface area of a sheet at which vorticity differs from zero in the limit of very large Reynolds numbers.
• This process is associated with certain values of the dimensionless parameter conventionally called skewness. Skewness usually has a measured value between 0.4 to 0.5 for developed turbulence. It is this growth of the surface area which is unambiguously related to the entropy growth.
• the vorticity surface growth through the formation of fractal can be seen as a manifestation of the second law of thermodynamics.
• the helicityassociated phases in the inertial range close to small dissipation scales are randomly shuffled, resulting in a destruction of fractal fine scale within the inertial range.
• the corresponding small scales thus become out of tune with the larger ones and diffusion through the volume of the medium results. Consequently, the fractal surface acquires width.
• the volume of vortical motion is an inviscid invariant due to Kelvin's Theorem of Circulation, the relevant area of fractal decreases.
• the growth of entropy at small scales is impeded and slowed, while the growth of entropy at small scales diminishes and more energy would stay at large scales whose organization also changes.
• a broad spectrum, stochastic external disturbance is introduced into the turbulent fluid medium wherein the maximum wavelengths of said disturbance are comparable to the Taylor microscale, or even larger scales in the inertial range of the turbulent flowing fluid.
• the disturbance should be introduced, in accordance with the present invention, into at least a portion of the inner part of the boundary layer adjacent the viscous sublayer.
• the term "inertial range” is likewise conventional and means the intermediate scales between the large energy containing and small dissipative scales.
• a characteristic scale of the inertial range is the Taylor microscale.
• the typical wavelength of the perturbation signal should be no larger than the Taylor microscale.
• the chaotic perturbation into the boundary layer can be in the form of an essentially white-noise disturbance whose center frequency is chosen such as to enhance propulsion of the vessel in the body of fluid by reducing the effects of turbulence.
• the fluid is conductive, such as sea water
• the noise is introduced into the boundary layer near the vessel surface by generating a time and space wideband varying electro-magnetic field in the boundary layer. Because of the conductivity of the water, the field interacts with the water causing a perturbation and randomization of the vortex lines in the boundary layer in synchronism with the excitation signal.
• the noise spectrum should preferably be chosen in conjunction with the turbulent energy spectrum.
• the result is that an inverse cascade of energy ensues and the dynamics of the coherent structures associated with large scale turbulence is disturbed thereby reducing small scale turbulence and dissipation in the boundary layer. Propulsion of the vessel in the water is thus enhanced by the expenditure of a small amount of energy in the perturbing magnetic field.
• the noise can be introduced into the boundary layer by generating a time and space varying wideband sonic signal within the boundary layer.
• the center wavelength of the sonic signal is comparable to the small-scale structure of the turbulence; and the sonic signal may be created using a series of transducers located on the wing surface of the aircraft, or in operative relationship thereto.
• an array of extensions such as small wires extending into the boundary layer may be excited under the combined action of the flow and their own elasticity in resisting the flow to provide the desired perturbation.
• an array of ferromagnetic extensions, such as wires, or additives such as particles moving in the boundary layer, being acted upon by a temporally and spatially varying high frequency electromagnetic field can be used to interact with the turbulent fluid and produce such excitations.

Landscapes

• Engineering & Computer Science (AREA)
• Physics & Mathematics (AREA)
• Fluid Mechanics (AREA)
• General Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Aviation & Aerospace Engineering (AREA)
• Mechanical Treatment Of Semiconductor (AREA)
• Physical Or Chemical Processes And Apparatus (AREA)
• Geophysics And Detection Of Objects (AREA)
• Nitrogen Condensed Heterocyclic Rings (AREA)
• Gas Separation By Absorption (AREA)
• Aeration Devices For Treatment Of Activated Polluted Sludge (AREA)
• Flow Control (AREA)
• Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Priority Applications (1)

Applications Claiming Priority (3)

Related Parent Applications (1)

Publications (1)

Family

ID=24195403

Family Applications (1)

Country Status (9)

Cited By (11)

Families Citing this family (4)

Citations (10)

• 1991
  • 1991-07-04 IL IL9874091A patent/IL98740A/xx active IP Right Grant
  • 1991-07-08 RU SU915001062A patent/RU2085764C1/ru active
  • 1991-07-08 UA UA5001062A patent/UA26128A/uk unknown
  • 1991-07-09 EP EP91306239A patent/EP0466468B1/en not_active Expired - Lifetime
  • 1991-07-09 AT AT91306239T patent/ATE159083T1/de active
  • 1991-07-09 DE DE69127860T patent/DE69127860T2/de not_active Expired - Fee Related
  • 1991-07-09 JP JP3168236A patent/JPH06241213A/ja active Pending
  • 1991-12-13 KR KR1019910011536A patent/KR100194909B1/ko not_active IP Right Cessation
• 1993
  • 1993-12-30 US US08/176,284 patent/US5354017A/en not_active Expired - Fee Related

Patent Citations (10)

Also Published As

Similar Documents

Legal Events